Credit
Vitaly V. Kuzmin · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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At a glance
9M119 Svir/Reflekslarger figure on 1 of 1
MILANlarger figure on 0 of 1
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Configuration
| Specification | 9M119 Svir/Refleks | MILAN |
|---|---|---|
| Type | ATGM[source] | Anti-tank missile[source] |
| Place of origin | Soviet Union[source] | France, West Germany[source] |
| In service | 1985–present[source] | 1972–present[source] |
| Used by | Soviet Union Russia China India Serbia South Korea[source] | See operators[source] |
Wingspan
Single source260 mm (10 in)[source]
Operational; Operational range · source measurement 1
Single sourceOperational; Operational range · source measurement 2
Single source4,000 / 5,000 m[source]
Operational; MILAN ER
Single sourceOperational; Operational range
Single sourceWarhead weight
Single source4.5 kg[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | First Chechen War Russo-Ukrainian War[source] | South African Border War Chadian-Libyan conflict Toyota War Western Sahara War Lebanese Civil War Iran–Iraq War Falklands War Gulf War 2003 invasion of Iraq Iraq War Opération Licorne Libyan Civil War Northern Mali Conflict Operation Sangaris War in Iraq (2013–2017) Syrian Civil War Russian invasion of Ukraine[source] |
|---|
| Designer | Tula Machinery Design Bureau (Tula KBP)[source] | — |
|---|
| Designed | 1980s[source] | 1970s[source] |
|---|
| Manufacturer | Degtyarev plant[source] | MBDA Also produced under license by: Bharat Dynamics (India) BAe Dynamics (United Kingdom)[source] |
|---|
| Unit cost | $37,500 (2012)[source] | £7,500 (1984)[source] |
|---|
| Produced | 1980s–present[source] | 1971[source] |
|---|
| Variants | 9M119M[source] | See variants[source] |
|---|
| Warhead | Tandem hollow-charge[source] | Single or tandem HEAT[source] |
|---|
| Guidance system | Laser beam riding[source] | SACLOS wire[source] |
|---|
| Launch platform | 125 mm smoothbore guns[source] | Individual, vehicle[source] |
|---|
| No. built | — | 350,000 missiles, 10,000 launchers[source] |
|---|
| Detonation mechanism | — | contact[source] |
|---|
| Engine | — | solid-fuel rocket[source] |
|---|
| Steering system | — | Jet deflector[source] |
|---|
| Reported operators |
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|
|---|
200–2,000 m (660–6,560 ft); 3,000 m (MILAN ER)[source]